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. Author manuscript; available in PMC: 2019 Oct 19.
Published in final edited form as: Annu Rev Fluid Mech. 2018 Jan;50:535–561. doi: 10.1146/annurev-fluid-122316-045241

Figure 5.

Figure 5

Cell count versus chord Reynolds number for spanwise-periodic airfoil simulations with an aspect ratio of 4; symbols denote the (scaled) cost of actual wall-modeled large-eddy simulation (WMLES) calculations of varying airfoils (NACA 0012, NACA 4412, Aerospatiale-A, NASA Common Research Model (CRM), and the MD 30P/30N), and lines denote Chapman’s cost estimates using nxnynz = 103 (green) and 203 (blue).